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| Autore: |
Connolly Joseph W
|
| Titolo: |
Loop Shaping control design for a supersonic propulsion system model using quantitative feedback theory (QFT) specifications and bounds [[electronic resource] /] / Joseph W. Connolly and George Kopasakis ; prepared for the 46th Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE, Nashville, Tennessee, July 25-28, 2010
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| Pubblicazione: | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010] |
| Descrizione fisica: | 1 online resource (19 pages) : illustrations (color) |
| Soggetto topico: | Supersonic flight |
| Control systems design | |
| Supersonic transports | |
| Specifications | |
| Supersonic inlets | |
| Dynamic models | |
| Loops | |
| Feedback control | |
| Supersonic wind tunnels | |
| Flow distribution | |
| Computational fluid dynamics | |
| Altri autori: |
KopasakisGeorge
|
| Note generali: | Title from title screen (viewed on June 13, 2011). |
| "October 2010." | |
| "AIAA-2010-7068." | |
| Nota di bibliografia: | Includes bibliographical references (pages 18-19). |
| Altri titoli varianti: | Loop Shaping control design for a supersonic propulsion system model using quantitative feedback theory |
| Titolo autorizzato: | Loop Shaping control design for a supersonic propulsion system model using quantitative feedback theory (QFT) specifications and bounds ![]() |
| Formato: | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione: | Inglese |
| Record Nr.: | 9910700358203321 |
| Lo trovi qui: | Univ. Federico II |
| Opac: | Controlla la disponibilità qui |